| タイトル | Static Testing of an Inflatable/Rigidizable Hexapod Structure |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040058058 |
| 著者（英） | Horta, L. G.; Taleghani, B. K.; Berger, K. T. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2004-04-02 |
| 言語 | eng |
| 内容記述 | Scientific application of large space antennas and telescopes is fostering the study of ultralightweight and inflatable structures. These so-called gossamer structures are tightly packaged for launch and subsequent deployment. Of particular interest is a hexapod configuration often found in vehicle ride simulators, ground-based telescopes, and antennas. One such configuration was modeled and tested at NASA Langley. Discrepancies between dynamic test data and predictions from a finite element model prompted additional static testing. This paper discusses static tests that were conducted to update stiffness parameters in the finite element model. |
| NASA分類 | Structural Mechanics |
| レポートNO | AIAA Paper 2004-1801 |
| 権利 | No Copyright |
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